View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 37084U 93036BFE 24276.40978794 .00018918 00000-0 16450-2 0 9997
2 37084 74.0326 324.6627 0112097 161.5660 198.9638 14.92143073597381
Epoch (UTC): | 02 October 2024 09:50:05 |
Eccentricity: | 0.0112097 |
inclination: | 74.0326° |
perigee height: | 513 km |
apogee height: | 669 km |
right ascension of ascending node: | 324.6627° |
argument of perigee: | 161.5660° |
revolutions per day: | 14.92143073 |
mean anomaly at epoch: | 198.9638° |
orbit number at epoch: | 59738 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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